Parten Clay, Subeshan Balakrishnan, Asmatulu Ramazan
Department of Mechanical Engineering, Wichita State University, 1845 Fairmount, Wichita, KS, 67260, USA.
Discov Nano. 2024 Jun 6;19(1):97. doi: 10.1186/s11671-024-04041-5.
The growing use of thermoplastic composites (TPCs) like low-melting polyaryletherketone (LM-PAEK) matrices reinforced with unidirectional carbon fiber (CF) in aircraft structures presents a significant challenge in terms of lightning strikes and electromagnetic interference shielding during aircraft operations. This is due to the weak electrical conductivity of TPC structures, which results in widespread damage when struck by lightning. The repair and maintenance of these extended damaged sites can increase operational costs and loss of flights. Several lightning strike protection (LSP) systems have been developed and implemented to address these concerns. This study evaluated a highly conductive coating with a low filler rate for its effectiveness as an LSP solution for TPCs on exterior aircraft surfaces. The TPC panel without any coatings was first studied. Subsequently, the level of conductivity was increased by incorporating the nanoscale conductive fillers, silver-coated copper (Ag/Cu) nanoflakes, with a silver content of 20 wt.% (Ag20/Cu) and 30 wt.% (Ag30/Cu), correspondingly, into the coating at two loadings of 55 wt.% and 70 wt.% in an epoxy carrier for the surface coatings. The behavior of electrical and surface conductivity was thoroughly examined to understand the impact of Ag/Cu with a high aspect ratio and the effectiveness of the LSP solution. In addition, the spray-coated TPC panels underwent rigorous Zone 2A lightning strike testing using simulated lightning current, in agreement with the industry standard of Society of Automotive Engineers (SAE) Aerospace Recommended Practice (ARP) 5412B. Despite the higher resistance due to the lower conductive coating weight, the TPC panels with Ag30/Cu at loading of 70 wt.% achieved better results than those with Ag30/Cu at loading of 55 wt.%. This is evidenced by the minor structural delamination and CF breakage on the front surface, which proposes a new economic route for a sustainable post-processed LSP system in the aviation industry.
在飞机结构中,热塑性复合材料(TPCs)如用单向碳纤维(CF)增强的低熔点聚芳醚酮(LM-PAEK)基体的使用日益增加,这在飞机运行期间的雷击和电磁干扰屏蔽方面带来了重大挑战。这是由于TPC结构的导电率较弱,导致在遭受雷击时会造成广泛损坏。这些大面积受损部位的修复和维护会增加运营成本并导致航班延误。为了解决这些问题,已经开发并实施了几种雷击防护(LSP)系统。本研究评估了一种低填料率的高导电涂层作为飞机外表面TPCs的LSP解决方案的有效性。首先研究了未涂任何涂层的TPC面板。随后,通过将纳米级导电填料、含银量为20 wt.%(Ag20/Cu)和30 wt.%(Ag30/Cu)的镀银铜(Ag/Cu)纳米片分别以55 wt.%和70 wt.%的两种负载量加入到用于表面涂层的环氧载体中,来提高导电率。对电导率和表面电导率的行为进行了深入研究,以了解高纵横比的Ag/Cu的影响以及LSP解决方案的有效性。此外,喷涂了涂层的TPC面板按照汽车工程师协会(SAE)航空航天推荐实践(ARP)5412B的行业标准,使用模拟雷电流进行了严格的2A区雷击测试。尽管由于导电涂层重量较低电阻较高,但负载量为70 wt.%的含Ag30/Cu的TPC面板比负载量为55 wt.%的含Ag30/Cu的TPC面板取得了更好的结果。这一点从正面表面较小的结构分层和CF断裂得到证明,这为航空业可持续的后处理LSP系统提出了一条新的经济途径。